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Projectiles that include a propulsion system and a launch motor which are located on opposing sides of a payload and a method of directing a projectile toward a target are generally described herein. Placing the propulsion system and the launch motor on opposing sides of the payload may provide many

Projectiles that include a propulsion system and a launch motor which are located on opposing sides of a payload and a method of directing a projectile toward a target are generally described herein. Placing the propulsion system and the launch motor on opposing sides of the payload may provide many potential advantages when designing the projectile. These design advantages may make it easier to create a projectile that includes more propellant and/or payload while still permitting the projectile to be stored within existing containers having a fixed size.

대표청구항 ▼

1. A projectile comprising: a payload;a launch motor that directs thrust from an aft end of the projectile;a propulsion system located on a fore end of the projectile, wherein the propulsion system and the launch motor are located on opposing sides of the payload, wherein the propulsion system inclu

1. A projectile comprising: a payload;a launch motor that directs thrust from an aft end of the projectile;a propulsion system located on a fore end of the projectile, wherein the propulsion system and the launch motor are located on opposing sides of the payload, wherein the propulsion system includes a nozzle oriented to direct thrust in an opposite direction to the thrust generated by the launch motor and lateral thrusters; andwherein a flight path of the projectile comprises: a first phase where the launch motor propels the projectile along the flight path; anda second phase where the launch motor is ejected from the projectile and the projectile is rotated such that the nozzle becomes an aft end of the projectile. 2. The projectile of claim 1 wherein the payload includes lateral thrusters that rotate the payload after the propulsion system has been ejected from the payload. 3. The projectile of claim 1 wherein the propulsion system includes a motor section attached to the payload and an expendable shroud attached to the motor section. 4. The projectile of claim 3 wherein the expendable shroud is a nose cone that is formed of a plurality of components such that the components are adapted to telescope inside one another. 5. The projectile of claim 3 wherein the motor section includes a cylindrical casing.